| contributor author | Linfa Zhu | |
| contributor author | Aditi Chattopadhyay | |
| contributor author | Robert K. Goldberg | |
| date accessioned | 2017-05-08T21:16:21Z | |
| date available | 2017-05-08T21:16:21Z | |
| date copyright | July 2008 | |
| date issued | 2008 | |
| identifier other | %28asce%290893-1321%282008%2921%3A3%28132%29.pdf | |
| identifier uri | http://yetl.yabesh.ir/yetl/handle/yetl/45118 | |
| description abstract | A modified Hashin failure model is developed to characterize different failure modes related to high-velocity impact of composite laminates. Hashin’s compressive fiber failure mode has been extended to consider the shear stress effect. Several micromechanics-based degradation rules are developed and applied to the stress and material property calculations according to different failure modes after the corresponding failure criterion is satisfied. This model has been implemented into a recently developed micromechanics model. Computational results show that this model is able to address shear failure, delamination, and tearing failure observed in the high-velocity impact of composite laminates. | |
| publisher | American Society of Civil Engineers | |
| title | Failure Model for Rate-Dependent Polymer Matrix Composite Laminates under High-Velocity Impact | |
| type | Journal Paper | |
| journal volume | 21 | |
| journal issue | 3 | |
| journal title | Journal of Aerospace Engineering | |
| identifier doi | 10.1061/(ASCE)0893-1321(2008)21:3(132) | |
| tree | Journal of Aerospace Engineering:;2008:;Volume ( 021 ):;issue: 003 | |
| contenttype | Fulltext | |